Finite element analysis of cohesive element for glass epoxy composite fuselage model
In this research, a numerical simulation on a newly introduced fabrication miniature composite fuselage structure - a glass epoxy composite laminated with adhesively bonded butt joint under axial compression loading is presented. A FEA via ABAQUS/Explicit is utilized to capture the complete compress...
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| 第一著者: | |
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| フォーマット: | 学位論文 |
| 言語: | English |
| 出版事項: |
2011
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| オンライン･アクセス: | http://psasir.upm.edu.my/id/eprint/41770/1/FK%202011%202R.pdf http://psasir.upm.edu.my/id/eprint/41770/ |
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